| The use of OH* and CH* as heat release markers in combustion dynamics S Sardeshmukh, M Bedard, W Anderson International Journal of Spray and Combustion Dynamics 9 (4), 409-423, 2017 | 89 | 2017 |
| Chemiluminescence as a diagnostic in studying combustion instability in a practical combustor MJ Bedard, TL Fuller, S Sardeshmukh, WE Anderson Combustion and Flame 213, 211-225, 2020 | 77* | 2020 |
| Self-sustained, high-frequency detonation wave generation in a semi-bounded channel K Schwinn, R Gejji, B Kan, S Sardeshmukh, S Heister, CD Slabaugh Combustion and Flame 193, 384-396, 2018 | 60 | 2018 |
| Prediction of combustion instability with detailed chemical kinetics SV Sardeshmukh, SD Heister, WE Anderson 53rd AIAA Aerospace Sciences Meeting, 1826, 2015 | 48 | 2015 |
| Transducer installation effects on pressure measurements in PGC devices RM Gejji, IV Walters, S Beard, A Lemcherfi, SV Sardeshmukh, SD Heister, ... 2018 AIAA aerospace sciences meeting, 0158, 2018 | 46 | 2018 |
| High-pressure rotating detonation engine testing and flameholding analysis with hydrogen and natural gas DP Stechmann, SD Heister, SV Sardeshmukh 55th AIAA Aerospace Sciences Meeting, 1931, 2017 | 45 | 2017 |
| Role of ignition delay in rotating detonation engine performance and operability DP Stechmann, S Sardeshmukh, SD Heister, K Mikoshiba Journal of Propulsion and Power 35 (1), 125-140, 2019 | 33 | 2019 |
| Tubular fuel injector for secondary fuel nozzle A Singh, SV Sardeshmukh US Patent 8,113,001, 2012 | 23 | 2012 |
| On the response of annular injectors to rotating detonation waves K Mikoshiba, SV Sardeshmukh, SD Heister Shock Waves 30 (1), 29-40, 2020 | 17 | 2020 |
| Effect of Aerospike Plug Nozzle Design on Rotating Detonation Engine Performance for Rocket Applications A Harroun, SD Heister, SV Sardeshmukh, JH Ruf AIAA Scitech 2019 Forum, 0197, 2019 | 16 | 2019 |
| High-pressure experiments relevant to rocket propulsion S Sardeshmukh, C Huang, R Gejji, M Bedard, Z Hallum, R Lucht, ... | 15 | 2020 |
| Sensitivity analysis of bluff-body stabilized premixed flame large-eddy simulations AL Comer, C Huang, S Sardeshmukh, BA Rankin, ME Harvazinski, ... Journal of Propulsion and Power 37 (2), 211-222, 2021 | 13 | 2021 |
| Impact of Chemical Kinetics Mechanisms on the Predictions of Bluff Body Stabilized Flames SV Sardeshmukh, C Huang, WE Anderson, ME Harvazinski, V Sankaran 54th AIAA Aerospace Sciences Meeting, 1687, 2016 | 13 | 2016 |
| Self-excited, multi-khz dynamics in a linear, semi-bounded detonation channel KS Schwinn, B Kan, SV Sardeshmukh, RM Gejji, SD Heister, ... 55th AIAA Aerospace Sciences Meeting, 0375, 2017 | 12 | 2017 |
| Combustion instability modeling using multi-mode flame transfer functions and a nonlinear Euler solver GMR Tamanampudi, S Sardeshmukh, W Anderson, C Huang International Journal of Spray and Combustion Dynamics 12, 1756827720950320, 2020 | 10 | 2020 |
| Comprehensive computational modeling of hypergolic propellant ignition S Sardeshmukh Purdue University, 2013 | 9 | 2013 |
| Kinetic modeling of hypergolic propellants using impinging element injectors S Sardeshmukh, S Heister, G Xia, C Merkle, V Sankaran 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3760, 2012 | 9 | 2012 |
| Flamelet modeling studies of a continuously variable resonance combustor T Pant, C Huang, C Han, SV Sardeshmukh, WE Anderson, H Wang 54th AIAA Aerospace Sciences Meeting, 1941, 2016 | 8 | 2016 |
| Reduced order modeling of rotational detonation engines J Humble, SV Sardeshmukh, SD Heister AIAA Scitech 2019 Forum, 0201, 2019 | 7 | 2019 |
| Kinetics modeling of hypergolic propellants SV Sardeshmukh, SD Heister, V Sankaran, H Wang 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 4157, 2013 | 7 | 2013 |
Cheng HuangUniversity of KansasVerified email at ku.edu
